Patents
Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
09/2002
09/12/2002CA2438156A1 Method for the plasma coating of a turbine blade or vane, and coating device
09/11/2002EP1239454A1 Method of manufacturing a panel with an adapted, acoustically resistive layer and resulting panel
09/11/2002EP1239131A2 Methods and apparatus for operating gas turbine engines
09/11/2002EP1239121A2 An air-cooled gas turbine exhaust casing
09/11/2002EP1239117A2 Gas turbine combustor transition piece outlet structure, transition piece, combustor and gas turbine
09/11/2002EP1239059A2 Chemical milling of the blades of a gas turbine engine
09/11/2002EP1238184A1 Machine set
09/11/2002EP1237641A1 Engine with upstream and rotationally attached guard
09/11/2002EP1169495A4 Electrochemical stripping of turbine blades
09/11/2002EP0891483B1 Closed-loop air cooling system for a turbine engine
09/10/2002US6447255 Gas turbine nose cone assembly
09/10/2002US6446440 Steam injection and inlet fogging in a gas turbine power cycle and related method
09/10/2002US6446437 Fuel system
09/06/2002WO2002068867A2 Control strategy for flexible catalytic combustion system
09/06/2002WO2002068800A1 Turbine blade with pre-segmented squealer tip
09/06/2002WO2002048508A3 Turbine bucket cover and brush seal
09/05/2002US20020123827 System and method for performing electronic triage of a turbine part
09/05/2002US20020122723 Electrical machine
09/05/2002US20020122717 Low drag ducted ram air turbine generator and cooling system
09/05/2002US20020122716 Methods and apparatus for cooling gas turbine engine blade tips
09/05/2002US20020122458 Utilization of pyrometer data to detect oxidation
09/05/2002US20020121091 Transient turbine exhaust temperature control for a turbogenerator
09/05/2002US20020121090 Gas turbine engine jet noise suppressor
09/05/2002US20020121082 Air-cooled gas turbine exhaust casing
09/05/2002US20020121080 Fluid flow control valve
09/05/2002DE10134612A1 Gas turbine assembly, for a power station, has coolants for the combustion air which also keep the critical turbine components at a temperature below the maximum heat safety levels
09/05/2002DE10108561A1 Thermische Turbomaschine und Verfahren zum Zünden der thermischen Turbomaschine A thermal turbo-machine and method for starting the thermal turbomachine
09/05/2002DE10104150A1 Brenneranlage und Verfahren zu ihrem Betrieb Burner system and method for its operation
09/04/2002EP1236864A2 System and method for perfoming electronic triage of a turbine part and for carrying out a turbine part repair
09/04/2002EP1236534A2 Method and fixture for disposing filler material in an article
09/04/2002EP1236197A1 Device for soundproof covering
09/04/2002EP0968355B1 Cooling supply manifold assembly for cooling combustion turbine components
09/04/2002EP0966594B1 Coal fuel gas turbine system
09/04/2002EP0880672B1 Capacitive gap measurement device
09/03/2002US6445995 Vibration sensing in gas turbine engine
09/03/2002US6443699 Bushing retention system for thermal medium cooling delivery tubes in a gas turbine rotor
09/03/2002US6443694 Rotor machine device
09/03/2002US6443213 System for casting a metal article using a fluidized bed
09/03/2002US6442945 Gas turbine engine
09/03/2002US6442944 Bleed air heat exchanger integral to a jet engine
09/03/2002US6442942 Supercharging system for gas turbines
09/03/2002US6442941 Compressor discharge bleed air circuit in gas turbine plants and related method
09/03/2002US6442940 Gas-turbine air-swirler attached to dome and combustor in single brazing operation
09/03/2002US6442930 Combined cycle pulse detonation turbine engine
09/03/2002US6442929 Igniter assembly having spring biasing of a semi-hemispherical mount
09/03/2002US6442927 Gas turbine for combined cycle power plant
09/03/2002US6442925 Manifold drain system for gas turbine
09/03/2002CA2264682C Gas turbine cooled blade tip shroud
09/03/2002CA2089272C Impact resistant combustor
08/2002
08/29/2002WO2002066324A2 Improved aircraft system architecture
08/29/2002WO2002066323A2 Improved aircraft architecture with a reduced bleed aircraft secondary power system
08/29/2002WO2002042150B1 Aircraft deicer
08/29/2002WO2002037046A3 Turbogenerator cooling system
08/29/2002WO2002018674A3 Thermal barrier coating system for turbine components
08/29/2002US20020117581 Low sonic boom inlet for supersonic aircraft
08/29/2002US20020117485 Method and apparatus for increasing welding rates for high aspect ratio welds
08/29/2002DE10155508A1 Verfahren und Vorrichtung zur Erzeugung von elektrischer Energie Method and apparatus for production of electric energy
08/28/2002EP1235010A2 Repositionable brush seal for turbomachinery
08/28/2002EP1234963A1 Turbomachine ignition device and ignition method
08/28/2002EP1234962A2 Gas turbine and method to cool the combustion air
08/28/2002EP1234144A1 Simple low cost fuel nozzle support
08/28/2002EP1234130A1 Heat-resistant magnetic silicone rubber body for brush seals in turbomachinery and methods of application
08/28/2002EP1234105A1 Sequential use of steam
08/28/2002EP1032779B1 Planetary gear
08/28/2002CN1089796C Dimethyl ether fuel and method of generating power in dry low NOx combustion system
08/27/2002US6439844 Turbine bucket cover and brush seal
08/27/2002US6439842 Gas turbine engine stator case
08/27/2002US6439841 Turbine frame assembly
08/27/2002US6439840 Bypass duct fan noise reduction assembly
08/27/2002US6439340 Acoustically treated structurally reinforced sound absorbing panel
08/27/2002US6439023 Methods and apparatus for retrofitting compressible flanges
08/27/2002US6438963 Liquid fuel and water injection purge systems and method for a gas turbine having a three-way purge valve
08/27/2002US6438962 System and method for starting an engine
08/27/2002US6438960 Engine stall and distortion suppression system
08/27/2002US6438958 Apparatus for reducing heat load in combustor panels
08/27/2002US6438940 Methods and apparatus for providing uniform ignition in an augmenter
08/27/2002US6438939 Combined cycle power plant and cooling steam supply method for gas turbine therein
08/27/2002US6438938 Bearing compartment self cooling vent system
08/27/2002US6438936 Recuperator for use with turbine/turbo-alternator
08/27/2002CA2284491C Combined cycle electric power plant
08/27/2002CA2262233C Gas turbine starting control system
08/22/2002US20020114701 Method of investment casting with casting identification
08/22/2002US20020114696 Gas turbine nozzle vane insert and methods of installation
08/22/2002US20020113167 Aircraft architecture with a reduced bleed aircraft secondary power system
08/22/2002US20020112483 Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure
08/22/2002US20020112481 Method and apparatus for removing alkali metal contamination from gas turbine liquid fuels
08/22/2002US20020112465 Methods and apparatus for water injection in a turbine engine
08/21/2002EP1233147A2 Gas turbine with cooling arrangement
08/21/2002EP1233146A2 Gas turbine nozzle vane insert and methods of installation
08/21/2002EP1233081A1 Process and apparatus for plasma coating a turbine blade
08/21/2002EP1232562A2 Induction static start for a turbine generator with a brushless exciter and associated methods
08/21/2002EP1231999A1 Filter arrangement and methods
08/21/2002EP0904512B1 Heat-shield arrangement, especially for structural components of gas turbine plants
08/21/2002CN1089408C Axial turbine of turbocharger
08/20/2002US6437535 Starting system and method for a microturbine power generation unit
08/20/2002US6435820 Shroud assembly having C-clip retainer
08/20/2002US6435816 Gas injector system and its fabrication
08/20/2002US6435814 Film cooling air pocket in a closed loop cooled airfoil
08/20/2002US6435812 Bore tube assembly for steam cooling a turbine rotor
08/20/2002US6434949 Method and treatment device for the cooling of highly heated metal components